Apparatus for heating hydrocarbons with RF antenna assembly having segmented dipole elements and related methods

ABSTRACT

The apparatus includes an RF antenna assembly to be positioned within a wellbore and coupled to an RF source. The RF antenna assembly includes a first tubular dipole element having opposing proximal and distal ends, an RF transmission line extending through the proximal end of the first tubular dipole element and including an inner conductor, an outer conductor, and a dielectric therebetween. The inner conductor extends outwardly beyond the distal end of the first tubular dipole element. The outer conductor is coupled to the distal end of the first tubular dipole element. The RF antenna assembly includes a second tubular dipole element having opposing proximal and distal ends, with the proximal end being adjacent the distal end of the first tubular dipole element and being coupled to the inner conductor, and a tubular balun.

FIELD OF THE INVENTION

The present invention relates to the field of hydrocarbon resourcerecovery, and, more particularly, to hydrocarbon resource recovery usingradio frequency (RF) heating.

BACKGROUND OF THE INVENTION

Energy consumption worldwide is generally increasing, and conventionalhydrocarbon resources are being consumed. In an attempt to meet demand,the exploitation of unconventional resources may be desired. Forexample, highly viscous hydrocarbon resources, such as heavy oils, maybe trapped in tar sands where their viscous nature does not permitconventional oil well production. Estimates are that trillions ofbarrels of oil reserves may be found in such tar sand formations.

In some instances these tar sand deposits are currently extracted viaopen-pit mining. Another approach for in situ extraction for deeperdeposits is known as Steam-Assisted Gravity Drainage (SAGD). The heavyoil is immobile at reservoir temperatures and therefore the oil istypically heated to reduce its viscosity and mobilize the oil flow. InSAGD, pairs of injector and producer wells are formed to be laterallyextending in the ground. Each pair of injector/producer wells includes alower producer well and an upper injector well. The injector/productionwells are typically located in the pay zone of the subterraneanformation between an underburden layer and an overburden layer.

The upper injector well is used to typically inject steam, and the lowerproducer well collects the heated crude oil or bitumen that flows out ofthe formation, along with any water from the condensation of injectedsteam. The injected steam forms a steam chamber that expands verticallyand horizontally in the formation. The heat from the steam reduces theviscosity of the heavy crude oil or bitumen which allows it to flow downinto the lower producer well where it is collected and recovered. Thesteam and gases rise due to their lower density so that steam is notproduced at the lower producer well and steam trap control is used tothe same affect. Gases, such as methane, carbon dioxide, and hydrogensulfide, for example, may tend to rise in the steam chamber and fill thevoid space left by the oil defining an insulating layer above the steam.Oil and water flow is by gravity driven drainage urged into the lowerproducer well.

Operating the injection and production wells at approximately reservoirpressure may address the instability problems that adversely affecthigh-pressure steam processes. SAGD may produce a smooth, evenproduction that can be as high as 70% to 80% of the original oil inplace (OOIP) in suitable reservoirs. The SAGD process may be relativelysensitive to shale streaks and other vertical barriers since, as therock is heated, differential thermal expansion causes fractures in it,allowing steam and fluids to flow through. SAGD may be twice asefficient as the older cyclic steam stimulation (CSS) process.

Many countries in the world have large deposits of oil sands, includingthe United States, Russia, and various countries in the Middle East. Oilsands may represent as much as two-thirds of the world's total petroleumresource, with at least 1.7 trillion barrels in the Canadian AthabascaOil Sands, for example. At the present time, only Canada has alarge-scale commercial oil sands industry, though a small amount of oilfrom oil sands is also produced in Venezuela. Because of increasing oilsands production, Canada has become the largest single supplier of oiland products to the United States. Oil sands now are the source ofalmost half of Canada's oil production, although due to the 2008economic downturn work on new projects has been deferred, whileVenezuelan production has been declining in recent years. Oil is not yetproduced from oil sands on a significant level in other countries.

According to the Alberta Research Council, a typical Athabasca oil sandmay contain 10 to 13 percent bitumen by weight, 3.5 to 8% percent waterby weight, with remainder sand and clay. The electrical conductivity at1 MHz may be 50 to 80 millimhos per meter, and the relative dielectricpermittivity may be 9 to 20 (i.e. dimensionless). The connate water andits associated electrical conductivity makes oil sand an excellentelectromagnetic heating susceptor, meaning it can heated with electricand magnetic fields at radio and microwave frequencies. U.S. PublishedPatent Application No. 2010/0078163 to Banerjee et al. discloses ahydrocarbon recovery process whereby three wells are provided, namely anuppermost well used to inject water, a middle well used to introducemicrowaves into the reservoir, and a lowermost well for production. Amicrowave generator generates microwaves which are directed into a zoneabove the middle well through a series of waveguides. The frequency ofthe microwaves is at a frequency substantially equivalent to theresonant frequency of the water so that the water is heated.

Along these lines, U.S. Published Patent Application No. 2010/0294489 toDreher, Jr. et al. discloses using microwaves to provide heating. Anactivator is injected below the surface and is heated by the microwaves,and the activator then heats the heavy oil in the production well. U.S.Published Patent Application No. 2010/0294488 to Wheeler et al.discloses a similar approach.

U.S. Pat. No. 7,441,597 to Kasevich discloses using a radio frequencygenerator to apply RF energy to a horizontal portion of an RF wellpositioned above a horizontal portion of an oil/gas producing well. Theviscosity of the oil is reduced as a result of the RF energy, whichcauses the oil to drain due to gravity. The oil is recovered through theoil/gas producing well.

Unfortunately, long production times, for example, due to a failedstart-up, to extract oil using SAGD may lead to significant heat loss tothe adjacent soil, excessive consumption of steam, and a high cost forrecovery. Significant water resources are also typically used to recoveroil using SAGD, which impacts the environment. Limited water resourcesmay also limit oil recovery. SAGD is also not an available process inpermafrost regions, for example. Slow, conducted heating may benecessary initially to soften the formation in order to permit theconvective flow of steam heat.

Moreover, despite the existence of systems that utilize RF energy toprovide heating, such systems may suffer from inefficiencies as a resultof impedance mismatches between the RF source, transmission line, and/orantenna. These mismatches become particularly acute with increasedheating of the subterranean formation. Moreover, such applications mayrequire high power levels that result in relatively high transmissionline temperatures that may result in transmission failures. High commonmode currents may also be generated on an outer conductor of a coaxialtransmission line that is unbalanced and that feeds a balanced antenna,such as a dipole, for example. For example, common mode currents maylead to unwanted heating in the overburden or at the surface.

SUMMARY OF THE INVENTION

In view of the foregoing background, it is therefore an object of thepresent invention to provide a RF heating apparatus that is efficientand robust.

This and other objects, features, and advantages in accordance with thepresent invention are provided by an apparatus for heating a hydrocarbonresource in a subterranean formation having a wellbore extendingtherein. The apparatus comprises an RF source, and an RF antennaassembly configured to be positioned within the wellbore and coupled tothe RF source. The RF antenna assembly comprises a first tubular dipoleelement having opposing proximal and distal ends, an RF transmissionline extending through the proximal end of the first tubular dipoleelement and comprising an inner conductor, an outer conductor, and adielectric therebetween. The inner conductor extends outwardly beyondthe distal end of the first tubular dipole element. The outer conductoris coupled to the distal end of the first tubular dipole element. The RFantenna assembly includes a second tubular dipole element havingopposing proximal and distal ends, with the proximal end being adjacentthe distal end of the first tubular dipole element and being coupled tothe inner conductor, and a tubular balun having the RF transmission lineextending therethrough and opposing proximal and distal ends, with thedistal end being adjacent the proximal end of the first tubular dipoleelement and the proximal end being coupled to the outer conductor.Advantageously, the apparatus may efficiently heat the hydrocarbonresources in the subterranean formation.

In some embodiments, the RF antenna assembly may comprise a tubularisolator having the RF transmission line extending therethrough andconfigured to couple together the tubular balun and the first tubulardipole antenna element. For example, the tubular isolator may comprise acyanate ester composite material.

Additionally, the RF antenna assembly may further comprise a feedstructure comprising a dielectric tube between the first and secondtubular dipole antenna elements, a first connector coupling the outerconductor to the first tubular dipole element, and a second connectorcoupling the inner conductor to the second tubular dipole element.Another aspect is directed to a method for making an RF antenna assemblyfor heating a hydrocarbon resource in a subterranean formation having awellbore extending therein. The method comprises providing a firsttubular dipole element having opposing proximal and distal ends, andpositioning an RF transmission line to extend through the proximal endof the first tubular dipole element. The RF transmission line comprisesan inner conductor, an outer conductor, and a dielectric therebetween.The inner conductor extends outwardly beyond the distal end of the firsttubular dipole element, the outer conductor to be coupled to the distalend of the first tubular dipole element. The method includes providing asecond tubular dipole element having opposing proximal and distal ends,with the proximal end being adjacent the distal end of the first tubulardipole element and coupled to the inner conductor, and positioning atubular balun to have the RF transmission line extending therethrough,the tubular balun having opposing proximal and distal ends, with thedistal end being adjacent the proximal end of the first tubular dipoleelement and the proximal end to be coupled to the outer conductor.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a schematic diagram of an apparatus, according to the presentinvention.

FIG. 2 is a schematic diagram of a portion of the RF antenna assemblyfrom the apparatus of FIG. 1.

FIG. 3 is a cross-section view of a portion of one embodiment of thefeed structure from the apparatus of FIG. 1 along line 3-3.

FIG. 4 is a diagram showing the measured heating performance of anexample embodiment of the apparatus from FIG. 1, in sandy soil.

FIG. 5 is a Smith diagram illustrating the measured load impedance of anexample embodiment of the apparatus from FIG. 1.

FIG. 6 is a diagram showing the measured RF power applied to an exampleembodiment of the apparatus of FIG. 1.

FIG. 7 is a diagram showing the realized subterranean temperaturesproduced by an example embodiment of the apparatus of FIG. 1 whileheating oil sand.

FIG. 8 is a diagram showing a double tuning method for the apparatus ofFIG. 1.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

The present invention will now be described more fully hereinafter withreference to the accompanying drawings, in which preferred embodimentsof the invention are shown. This invention may, however, be embodied inmany different forms and should not be construed as limited to theembodiments set forth herein. Rather, these embodiments are provided sothat this disclosure will be thorough and complete, and will fullyconvey the scope of the invention to those skilled in the art. Likenumbers refer to like elements throughout.

Referring initially to FIGS. 1-2, an apparatus 10 according to thepresent invention is now described. The apparatus 10 is for heating ahydrocarbon resource in a subterranean formation 17 having wellboresextending therein. The apparatus includes an injector well 11, and aproducer well 12 extending into respective wellbores in the subterraneanformation 17. The apparatus 10 comprises an RF source 13 coupled to theinjector well 11, and the injector comprises an RF antenna assembly 24to be positioned within the wellbore.

The RF antenna assembly 24 comprises a first tubular (sleeve) dipoleelement 81a having opposing proximal 21 and distal 22 ends. As usedherein, distal means deeper into the wellbore while proximal meanstowards the surface. The RF antenna assembly 24 comprises an RFtransmission line 82, such as a shielded RF transmission line or acoaxial RF transmission line, extending through the proximal end 21 ofthe first tubular dipole element 81a and comprising an inner conductor72, an outer conductor 71, and a dielectric 73 therebetween. The innerconductor 72 extends outwardly beyond the distal end 22 of the firsttubular dipole element 81a. The outer conductor 71 is coupled to thedistal end 22 of the first tubular dipole element 81a, illustrativelyshown as a closed end connection, i.e., this end of the tube is capped.The RF antenna assembly 24 includes a second tubular (sleeve) dipoleelement 81b having opposing proximal 27 and distal 28 ends. The proximalend 27 of the second tubular dipole element 81b is adjacent the distalend 22 of the first tubular dipole element 81a and is coupled to theinner conductor 72. The RF antenna assembly 24 includes a tubular(sleeve) balun 15 having the RF transmission line 82 extendingtherethrough and opposing proximal 25 and distal 26 ends. The distal end26 of the tubular balun 15 is adjacent the proximal end 21 of the firsttubular dipole element 81a, and the proximal end 25 of the tubular balun15 is coupled to the outer conductor 71, illustratively shown as aclosed end connection.

In the illustrated embodiment, the RF antenna assembly 24 comprises atubular isolator 31 having the RF transmission line 82 extendingtherethrough and configured to couple together the tubular balun 15 andthe first tubular dipole antenna element 81a. The tubular isolator 31provides an electrical discontinuity in the RF antenna assembly 24, atwhich RF electrical currents are supplied to the first and secondtubular (sleeve) dipole elements 81a, 81b. For example, the tubularisolator 31 may comprise a cyanate ester composite material (e.g. quartzenhanced), polyimide, or to another suitable dielectric composite thathas mechanical strength for structural integrity, and absorbs minimalamounts of radiated energy.

Advantageously, the tubular balun 15 is tuned to prevent RF energy frompenetrating uphole to the overburden and to concentrate heating downholetowards the hydrocarbon resources. As the subterranean formation 17heats, its electrical properties may change. So, the dipole tuning maydrift away from balun tuning. The overburden may not heat, so the balun15 tuning may not drift all. Separate tubular balun 15 and first tubulardipole antenna element 81a allow independent tuning to manage thistuning drift, i.e. there is a split of the tuning of the tubular balunand the antenna to deal with the different behavior of the overburdenand the hydrocarbon resources. In short, the region between the firsttubular dipole antenna element 81a and the tubular balun 15 is notheated.

So a method of the invention is the split tuning of the balun and theantenna to deal with the different behavior of the overburden. In thesplit tuning method: 1) the resonance of the first and second tubulardipole elements 81a, 81b is allowed to drift with heating; 2) RF source13 frequency is varied to track the drilling resonant frequency of thefirst and second tubular dipole elements 81a, 81b; and 3) tubular balun15 resonant frequency is adjusted by a tubular balun 15 tuning system,such as that described in co-pending patent application titled: “SYSTEMINCLUDING TUNABLE CHOKE FOR HYDROCARBON RESOURCE HEATING AND ASSOCIATEDMETHODS,” U.S. patent application Ser. No. 13/657,172 filed Oct. 22,2012, the contents of which are hereby incorporated by reference intheir entirety.

Additionally, the apparatus 10 comprises a tubular ferrite choke 16surrounding the RF transmission line 82 and spaced apart from theproximal end 25 of the tubular balun 15. The first and second tubulardipole elements 81a-81b have a desired operating frequency, and each ofthe first tubular dipole element, the second tubular dipole element, andthe tubular balun 15 may have a length corresponding to +/−10% of aquarter of a wavelength of the desired operating frequency, i.e. thefirst and second tubular dipole elements form a half-wave dipoleantenna, as illustratively noted in FIG. 2. Moreover, as alsoillustrated in FIG. 2, the current flows in the RF antenna assembly 24are shown with arrows. Advantageously, the current from the outerconductor 71 does not penetrate the tubular balun 15.

In FIG. 2, the arrows I denote the flows of RF current at an instant intime, at a preferred electrical size, where the first tubular dipoleelement 81a is one quarter wavelength (λ/4) in length and the secondtubular dipole element 81b is also one quarter wavelength (λ/4) inlength. The tubular dipole elements 81a-81b carry a sinusoidal electriccurrent that converges and diverges from tubular isolator 31. Theinternal surfaces of the tubular balun 15 and the first tubular dipoleelement 81a both comprise coaxial stubs, which carry internal currentsthat do not provide subterranean formation 17 heating, but are otherwiseuseful to provide common mode current suppression and underground tuningcomponents. The present embodiments are not so limited however as toonly be operated at ¼ wavelength electrical dimensions for the first andsecond tubular dipole elements 81a, 81b.

Referring now additionally to FIG. 3, the RF antenna assembly 24 furthercomprises a feed structure 50 coupling together the first and secondtubular dipole antenna elements 81a-81b and electrically coupling the RFtransmission line 82 and the first and second tubular dipole antennaelements. The feed structure 50 includes a dielectric tube 61 betweenthe first and second tubular dipole antenna elements 81a-81b, a firstconnector 60a coupling the outer conductor 71 to the first tubulardipole element, and a second connector 60b coupling the inner conductor72 to the second tubular dipole element. For example, the dielectrictube 61 may comprise a cyanate ester composite material (e.g. quartzenhanced) or another suitable dielectric composite that has mechanicalstrength for structural integrity, and absorbs minimal amounts ofradiated energy.

In the illustrated embodiment, the first and second connectors 60a-60binclude a plurality of tool-receiving recesses 65a-65b on an outersurface thereof. The tool-receiving recesses 65a-65b are illustrativelycircular in shape, but in other embodiments, may comprise other shapes,such as a hexagonal shape. The tool-receiving recesses 65a-65b areprovided to aid in using torque wrenches in assembling the antennaassembly 24. The RF transmission line 82 is affixed to the firstconnector 60a with a plurality of bolts 53a-53b. Of course, otherfasteners may be used.

In the illustrated embodiment, the inner conductor 72 comprises a tubedefining a first fluid passageway 85 therein. The outer conductor 71 isillustratively spaced from the inner conductor 72 to define a secondfluid passageway 73. The passageways 85, 73 permit the flow of selectivegases and fluids that aid in the hydrocarbon recovery process.

The feed structure 50 includes an intermediate conductor 62 extendingwithin the dielectric tube 61 and coupling the inner conductor 72 to thesecond connector 60b. For example, the intermediate conductor 62illustratively comprises a conductive tube of a material comprising,e.g., copper, aluminium. Moreover, the RF transmission line 82 includesan inner conductor coupler 67 for coupling the inner conductor 72 to theintermediate conductor 62, and first and second dielectric spacers74-75, each comprising a bore therein for receiving the inner conductorcoupler. Additionally, the first and second tubular dipole elements81a-81b each comprises a threaded end 63a-63b, and the first and secondconnectors 60a-60b each comprises a threaded end 86a-86b engaging arespective threaded end of the first and second tubular dipole elementsfor defining overlapping mechanical threaded joints 64a-64b. Thethreaded ends 63a-63b of the first and second tubular dipole elements81a-81b each comprises a mating face adjacent the first and secondconnectors 60a-60b. The mating face includes a threading relief recessto provide good contact at the outer extreme of the first and secondconnectors 60a-60b. The overlapping mechanical threaded joints 64a-64bprovide for a hydraulic seal that seals in fluid and gases within theantenna assembly 24.

Each of the first and second connectors 60a-60b comprises a recess66a-66b for receiving adjacent portions of the dielectric tube 61. Inthe illustrated embodiment, each recess comprises a circular slot thatis circumferential with regards to the first and second connectors60a-60b. Moreover, all edges in the illustrated embodiment are rounded,which helps to reduce arching in high voltage applications.

Another aspect is directed to a method for making an RF antenna assembly24 for heating a hydrocarbon resource in a subterranean formation 17having a wellbore extending therein. The method comprises providing afirst tubular dipole element 81a having opposing proximal and distalends 21, 22, and positioning an RF transmission line 82 to extendthrough the proximal end of the first tubular dipole element. The RFtransmission line 82 comprises an inner conductor 72, an outer conductor71, and a dielectric 73 therebetween. The inner conductor 72 extendsoutwardly beyond the distal end 22 of the first tubular dipole element81a, the outer conductor 71 to be coupled to the distal end 22 of thefirst tubular dipole element. The method includes providing a secondtubular dipole element 81b having opposing proximal and distal ends27-28, with the proximal end being adjacent the distal end 22 of thefirst tubular dipole element 81a and to be coupled to the innerconductor 72, and positioning a tubular balun 15 to have the RFtransmission line 82 extending therethrough, the tubular balun havingopposing proximal and distal ends 25-26, with the distal end beingadjacent the proximal end 21 of the first tubular dipole element and theproximal end to be coupled to the outer conductor.

A theory of operation for the apparatus 10 will now be provided. Thefirst and second tubular dipole elements 81a, 81b form the half elementsof a dipole antenna that is linear, e.g. line shaped for the divergenceof electric current. An inset feed is provided by concentricallylocating the RF transmission line 82 inside the first tubular dipoleelement 81a, advantageously allowing the RF well heater to be configuredin a single hole. Electrical charge is separated across the drivingdiscontinuity of the tubular isolator 31, which in turns causes acurrent flow along the first and second tubular dipole elements 81a,81b. Initially, if uninsulated from the subterranean formation 17, thefirst and second tubular dipole elements 81a, 81b act as electrodes tosupply electrical currents to the subterranean formation, which may thenbe the predominant mode of heating. The initial extension of the RFelectric currents axially along the first and second tubular dipoleelements 81a, 81b may be proportional to the RF skin depth or slightlymore than the RF skin depth. The RF skin effect therefore initiallyconcentrates the resistive, Joule effect heating to the vicinity of thetubular isolator 31. The connate water in the subterranean formation 17quickly turns to steam, so a steam saturation zone or “steam bubble”forms there. In this steam saturation zone, there may be rock, sand,hydrocarbons and vapor phase water, but no liquid water. The steambubble may be elongated as it grows from the center outwards followingalong the first and second tubular dipole elements 81a, 81b. Inparticular, at the steam bubble boundary along the first and secondtubular dipole elements 81a, 81b, where the liquid water still touchesthe first and second tubular dipole elements, there are hotspots ofheat. Thus, two moving hotspots of heat travel from tubular isolator 31outwards, the first traveling along the first tubular dipole element81a, and the second hotspot traveling along the second tubular dipoleelement 81b. Eventually, the moving hotspots reach the ends of the firstand second tubular dipole elements 81a, 81b, resulting in the first andsecond tubular dipole elements 81a, 81b becoming electrically insulatedfrom the subterranean formation 17 in a steam saturation zone. Steam isan electrical insulator whereas liquid water is an electrical conductor.When insulated from the subterranean formation 17, the energiesdelivered to the subterranean formation by the RF antenna assembly 24automatically shift from conducted electric currents to radiation ofelectric and magnetic fields. Thus the heating provided by the presentembodiments is reliable.

Continuing the theory of operation, the electric fields transduced fromthe insulated first and second tubular dipole elements 81a, 81bcapacitively couple the currents from those elements through the steambubble and into the liquid water regions beyond. In other words, firstand second tubular dipole elements 81a, 81b are in a sense akin tocapacitor plates. When the electric fields reach the connate liquidwater, they cause electrons to flow there, and this induced current flowheats the water resistively by Joule effect. Thus, capacitive couplingby transduced and radiated electric fields provides a means ofelectrical resistance heating in the subterranean formation 17 withoutthe need for electrode like conductive contact. This may be advantageousas electrode contact in hydrocarbon formations may be unreliable.

The diverging and oscillating flow of RF electric currents along thefirst and second tubular dipole elements 81a, 81b also transduce andradiate magnetic fields into the subterranean formation 17. As themagnetic fields expand through the connate water regions of thesubterranean formation 17, they initiate the flow of Eddy electriccurrents that heat the subterranean formation 17 by the Joule effect.Thus, magnetic field heating occurs by a compound, inductive process ofstarting with RF current flow on the first and second tubular dipoleelements 81a, 81b, followed by magnetic field expansion according toAmpere's Law, followed by Eddy current flow according to Lent's Law, andfinally formation heating by Joule effect. In a simple sense, inductionheating is akin to the RF antenna 24 being a current transformer primarywinding and the Eddy currents in the subterranean formation 17 beingcurrent transformer secondary windings, although these “windings” do notexist in a traditional sense. It may be typical that a wire coil isnecessary to cause magnetic induction heating, but a linear, line shapedelectric conductor also provides a useful, curling magnetic field for RFheating. The linear, line-shaped dimensions of the present embodimentsare more practical to install in the earth than a large diameter coil.

Continuing the theory of operation, if the first tubular dipole element81a is one quarter wavelength (λ/4) in length, and the second tubulardipole element 81b is also one quarter wavelength (λ/4) in length,magnetic field induction heating may be more prevalent near the centerof the RF antenna assembly 24, and electric field induction heating moreprevalent near the ends of the first and second tubular dipole elements81a, 82a. This is because the current and voltage distribution may besinusoidal with current maxima at the center of the dipole and voltagemaxima at the ends of the dipole. The electric and the magnetic fieldsprovided by the RF antenna assembly 24 work together to provide acontinuous heated area which may be an oblate spheroid or footballshape. At close ranges to the dipole, less than about λ_(media)/2π, thenature of the magnetic and electric fields may be those of reactive nearfields, and at extended ranges from the dipole, radii greater that aboutλ_(media)/2π, the transduced electric and magnetic fields may be thoseof a radio waves. Advantageously, both reactive near fields and theradio waves provide heating and the radio waves allow the heating tocontinue to virtually unlimited ranges. RF heating may not rise likesteam convection heating, so with RF heating caprock may not be requiredover the payzone.

Furthermore, realized temperatures underground are a function of theapplied RF power in kilowatts (KW), the heating duration in hours H, theheated mass in kg, and the specific heat of the subterranean formation17 in Joules per kilogram degree Kelvin (J/kg·K) or KW/kg·K. Thepenetration or radial thermal gradient surrounding the RF antennaassembly 24 is a function of both subterranean electrical conductivityin mhos/meter and of electromagnetic field expansion. Specifically,where r is the radius radially away from the axis of the RF antennaassembly 24, a 1/r² RF power gradient must occur away from a insulatedRF antenna 24 due to the spherical spreading of the RF fields, plus adissipative RF power gradient must occur due to the RF heating, whichmay be between 1/r³ to 1/r⁵ depending on subterranean formation 17electrical conductivity. Thus, the combined radial RF power gradient,spreading loss plus dissipative loss, may be 1/r⁵ to 1/r⁷. A practicalexample is that the instantaneous half depth of penetration of theelectromagnetic heating energies radially away from the apparatus 10 inrich oil sand of 0.005 mhos/meter electrical conductivity may be about20 inches. This is considerably superior to the initial, instantaneouspenetration of convected heating, which is zero or nearly zero. An RFheated zone can grow in size much more quickly than a steam injectionheated zone. Convective flow is not needed for RF heating to occur, andRF heating can heat impermeable structures, such as shale strata (andeven fracture the shale strata). Indeed, speed is a well known attributeof RF heating in general. The realized temperatures T of the RF heatingmay be any between the formation temperature prior to the commencementof the heating, to the boiling point of the connate subterranean waterat reservoir conditions, which may be 200° C. or more depending on depthand pressure. Thus the realized temperatures with the RF heatingregulate themselves so as not to exceed the boiling point of water atreservoir conditions. This advantageously avoids hydrocarbon cokingwhich may reduce subterranean formation permeability. RF heating mayalso prevent the deposit of varnishes on the well apparatus when liveoils are produced, as the oils will not be cooling as they drain.

The present embodiments are not so limited to require forming a steamsaturation zone underground, nor do they require that the subterraneantemperatures reach the boiling point of water. For instance, therealized temperatures may be reduced by reducing RF power levels.Another way to reduce realized temperatures, and a method of the presentdisclosure, is to inject critical fluids, such as alkane hydrocarbonsinto the subterranean formation 17 and allow the RF heating to drivethem. Injected alkanes may function to thermally regulate the extractionprocess at lower temperatures and act as a solvent to thin payzonehydrocarbons. Alkane molecules for injection may preferentially includepropane, butane, pentane, and hexane, which may boil below the boilingpoint of water. With alkane injection, the number of carbons in thealkane molecule may adjust the alkane boiling point, which in turn mayadjust the underground temperatures necessary to extract thesubterranean formation 17 hydrocarbons. The RF antenna assembly 24 mayinject the alkane solvent or a separate injector well may be provided,such as an infill well.

Moreover, although an advantageous mode of subterranean heating has beenidentified as Joule effect, the present embodiments are not so limited,and the introduced electric fields may also cause dielectric heating.Dielectric heating especially occurs due to the interaction of theelectric fields with polar molecules, particularly connate water. Thecombination of Joule effect and the dielectric heating allow the presentembodiments to operate effectively over a broad range of radiofrequencies, even near the dielectric heating minima frequency forwater, which occurs in the radio spectrum near 30 MHz. Preferred radiofrequencies for the present embodiments may therefore be between 40Hertz and 40 Megahertz. The higher frequencies may supply more loadresistance while lower frequencies may supply somewhat greaterpenetration. It may be advantageous to operate the apparatus 10 at aresonance frequency, fundamental or harmonic, of the dipole that isformed by the first and second tubular dipole elements 81a, 81b, asresonant operation may avoid a reactive or high power factor load, forinstance. Operation at harmonic resonance frequencies may provideresonant operation with alternative load resistances that mayadvantageously be higher or lower than the fundamental frequency loadresistance.

Continuing the theory of operation, hydrocarbons and water often occurtogether underground. When they do, RF electric and magnetic fields willheat subterranean water much faster than associated hydrocarbons. In thecase of oil sand, the connate pore water in oil sand RF generally heatsmore than 100 times faster than the bitumen. Thus, the pore waterbecomes hot first and then it conductively heats the bitumen films onthe pores. As the sand grains are many, the water pores small, and thebitumen pore films having substantial area and contact with the porewater, the rise in bitumen temperature closely paces the pore watertemperature rise. The bitumen may be melted and mobilized from anexpanding thermal front surrounding the apparatus 10 and if theunderground boiling temperatures are reached, the steam from the RFheated connate water may provide an additional driving to force tomobilize the warmed and thinned bitumen. Thus apparatus 10 may producehydrocarbons and connate water together at same time. If alkane solventsare injected, they may also provide a driving force to mobilize bitumen.Of course, hot water or injected steam can be provided as a pressuredrive on the hydrocarbons, and gravity drainage may also beincorporated. The speed and penetration of RF heating is much greaterthan that of steam heating, so RF electromagnetic heating providesincreased present value.

Electrical start up methods for the apparatus 10 will now be discussed.The RF antenna assembly 24 may be configured to initially provideconductive electrical contact with the subterranean formation 17 or itmay be electrically insulated from the formation initially. Both thebare and insulated approaches will be successful due to the many heatingmodes mentioned previously. However, an uninsulated RF antenna assembly24 may initially present a low resistance and high voltage standing waveratio (VSWR) until the connate water boils off, so an electrical startup my be needed. Various methods of start up are anticipated. Oneexemplary method of startup, winch has been tested, has been to supplyRF power into the low load resistance/high VSWR at reduced RF poweruntil the water boiled off the surfaces. Most RF power sources willmanage ill conditioned load impedances at low power, and only low poweris needed to boil the water off.

Another start up method is to elevate frequency until an increased loadresistance/low VSWR is obtained, as raising the frequency increases theload resistance when there is liquid water contact. Another startupmethod is to initially apply direct current (DC) to the RF antennaassembly 24 to boil the connate water off the antenna surfaces, as VSWRlosses do not occur at DC. Of course, the various methods to insulatethe RF antenna assembly 24 also exist, such as filling the hole with anonconductive material, eliminating the need for an electrical startupall together.

The tubular balun 15 may be provided to control or prevent common modecurrents. Here, a common mode current is defined as an electricalcurrent flowing on the outside of the RF transmission line 82. This mayoccur as the outer conductor 71 can support separate electrical currentflows on its inside and outside surfaces due to RF skin effect. Withoutthe tubular balun 15 then, stray capacitance between the uphole end ofthe first tubular dipole antenna elements 81a and the outer conductor 71may convey the RF heating currents uphole, through overburden, and evento the surface. This would be unwanted as heating in overburden may beuneconomic. RF heating at the surface may melt permafrost or even causea personnel safety hazard. The tubular balun 15 prevents these unwantedconditions by providing a high electrical resistance across its open endat radio frequencies. The high electrical resistance across the openmouth of the tubular balun 15 occurs due to the short circuit at theclosed end of the tubular balun 15 being referred to as an open circuitby the ¼ wavelength (or a odd harmonic of ¼ wavelength) length of thetubular balun. The short circuit end is referred as an open circuit (ornearly so) at the open end due the cosine distribution of current andsine distribution of voltage along the inside the tubular balun 15. Apreferred length of the tubular balun 15 is given by:L=0.25nλ/√μ_(r)∈_(r);where:

-   L=the physical length of the tubular balun 15, in meters;-   n=odd integers, e.g. 1, 3, 5 . . . ;-   λ=wavelength in meters=speed of light in meters per second/radio    frequency in Hertz;-   λ_(r)=relative magnetic permeability of fill inside tubular balun    15, if any; and-   ∈_(r)=relative dielectric permittivity of fill inside tubular balun    15, if any.

Referring now additionally to FIG. 4, diagram 90 illustrates themeasured heating performance of an example embodiment of the apparatus10 in a hill of sandy, moist soil which corresponded to a subterraneanformation 17. The sandy soil did not contain hydrocarbons but theelectrical and thermal characteristics of the sandy soil were similar tothose of rich oil sand, and in specific, the sandy soil had anelectrical conductivity of between σ=0.003 mhos/meter and 0.0005mhos/meter. The moist sand test was instrumented with temperature andpressure sensors at different distances from the RF antenna assembly 24.In particular, the diagram 90 illustrates performance at a time point of44 hours during a 5 day RF heating staging test.

Curve 91 shows the realized temperature profile immediately aside the RFantenna assembly 24 as a function of axial position along the RF antennaassembly. In the diagram 90, the RF antenna assembly 24 exited the sandhill at an axial position of 0 meters, and the downhole end of the RFantenna assembly 24 was at 35 meters. Curves 92-93 show the temperatureprofiles at 1 meter and 2.5 meters radial distance away film the RFantenna assembly 24. During the staging test, the example embodiment ofthe apparatus 10 radiated 86 kilowatts (KW) of power with a voltagestanding wave ratio of 3.06:1. Temperature peaks 94, 95 were caused byelectric fields at the ends of the first and second tubular dipoleantenna elements 81a-81b, which capacitively coupled electric currentsinto the moist sand nearby. Temperature peak 96 corresponded to thelocation of the tubular isolator 31 as locally increased electric fieldstrengths also existed there. Heating at local minimas 97, 98 was mostlydue to magnetic near fields from the first and second tubular dipoleantenna elements 81a-81b causing induced eddy currents in thesubterranean formation 17. Likewise, the longer range heating at the 1and 2.5 meter radii were also caused by magnetic fields from first andsecond tubular dipole antenna elements 81a-81b.

In general, magnetic field beating predominated at greater radialdistances. Note that unwanted uphole RF heating was effectivelyprevented by the tubular balun 15, so the RF heating was concentratedaround the first and second tubular dipole antenna elements 81a, 81b,located between 5 and 18 meters position. Temperature rise near thesurface, between about 0 and 5 meters axial position, was due to the sunand warm rain, which occurred during the test. At the time the test wasterminated, the RF heated zone was continuing to grow in size and theheating could have been extended. After the RF heating test, a hole wasdug into the top of the sand pile and steam rose there. Aninfrared/thermal camera clearly showed the heating region of the sandpile from a distance. An RF heated zone of virtually any required sizemay be created by the RF antenna assembly 24.

The apparatus 10 was later deployed in an undisturbed bench of rich ofoil sand, which contained bitumen. The intent of the oil sand test wasto demonstrate RF heating only, so a producer well and injected solventswere not provided. However, the borehole was much larger in diameterthan the apparatus 10 and, after RF heating, the free space filled withoil and leakage had to be contained. The driving force to mobilize theproduced oil was created by the RF fields, as no steam was injected. Theheating due to the electromagnetic fields mobilized the oil radiallyinwards. Table 1 below describes the measured results of the oil sandheating test with the apparatus 10.

TABLE 1 Oil Sand Test Results Parameter Value Subterranean formation 17Undisturbed bench of rich oil sand/bitumen ore. Ore electrical 0.002 to0.01 mhos/meter conductivity RF antenna assembly 24 Horizontalorientation RF antenna assembly 24 Double tuned half wave electricaltype dipole Borehole diameter 0.50 meters First and second tubular 0.15meters dipole element diameter 81a, 81b First and second tubular 10.6meters each dipole element length 81a, 81b First and second tubularAluminum dipole element length 81a, 81b material Tubular balun 15 length10.6 meters Tubular balun 15 diameter 0.15 meters Tubular balun 15diameter Aluminum material Dielectric conduit 0.33 meters diameter Outercasing The apparatus 10 was located inside a nonconductive dielectricconduit Outer casing material Isocyanurate polymer with spun glassfibers RF transmission line 82 Coaxial, formed of concentric tubing RFtransmission line 82 50 Ω characteristic impedance RF transmission line82 Recirculated dry nitrogen cooling and inerting Radio frequency 6.78MHz, held constant throughout the test Electromagnetic heating Inductionof electric mode currents by application of electric and magnetic fieldsPrimary heating mechanism Joule effect in connate water Secondaryheating Dielectric heating in mechanism connate water Solvent injectionNone Radiated RF power 0 to 50 kilowatts, varied throughout the test,see FIG. 6 Applied RF waveform Sinusoid (no modulation or pulses) RFsource 13 Modified shortwave broadcast transmitter RF source 13 activeTetrode vacuum tube, Eimac devices 4CV100,000C Duration of RF heating 35days Initial temperature of oil 4 to 10 degrees Celsius sand Endingtemperature of oil 120 degrees Celsius near sand the RF antenna assembly24, plus radial thermal gradient beyond Producer well Not providedProduced oil quantity 600-1000 gallons, estimatedOf course, more oil could have been produced if producer well wereprovided, solvents injected, steam introduced, etc.

Continuing the description of the oil sand test of the apparatus 10, anonconductive conduit was used to house the RF antenna assembly 24. Thenonconductive dielectric conduit was provided at the oil sand test toeasily slide the RF antenna assembly 24 in and out d the earth,especially after heating had occurred. Thus, no electric currents wereapplied to the hydrocarbon ore by electrode contact. A nonconductiveconduit is not required for the operation of the RF antenna assembly 24.

Furthermore, referring now additionally to FIGS. 5-6, diagram 120 showsthe measured electrical impedance of the RF antenna assembly 24 as theRF heating progressed. The diagram 120 is in a polar format known as aSmith Chart©, and it shows the measured electrical load that the RFantenna assembly 24 presented to the RF source 13 at the RF power source13, thus the phase delay of the RF transmission line 82 is included inthe measured impedance trace 122. The data points that make up trace 122represent different points in time, radio frequency was held constantthroughout the test. Point 124 was the initial impedance prior to thestart of the RF heating, and it measured to be Z=59+32j ohms or theequivalent of 59 ohms of resistance in series with 32 ohms of inductivereactance. Point 126 is the impedance at the conclusion of the RFheating on day 32, and it was measured to be Z=29−4j ohms or theequivalent of 29 ohms of resistance in series with 4 ohms of capacitivereactance. Circle 128 encloses the region of the Smith Chart having a 2to 1 VSWR or less.

Thus, the RF antenna assembly 24 advantageously maintained a VSWR of 2to 1 or less throughout the RF heating, providing a useful load for theRF source 13 whose impedance mismatch loss was 4 percent or less. The RFantenna 24 is a highly efficient RF heating applicator. More than 95percent of the RF power shown in FIG. 6 was delivered into the oil sand.The RF antenna assembly 24 impedance was measured by momentarily turningoff the RF power source 13 and connecting the vector network analyzer tothe RF antenna 24.

Continuing the oil sand test description, FIG. 6 graph 130 and trace 132depicts the RF power level that was applied to the RF antenna assembly24 over time. It became necessary to reduce the RF power level to reducethe amount of oil being produced. At the 50 kilowatt power level, theapplied power metric was 2.4 kilowatts/meter of well length.

Referring now additionally to FIG. 7, diagram 140 illustrates themeasured realized subterranean temperatures at the completion of the oilsand test of the example embodiment of the apparatus 10. Curve 142 showsthe realized temperature profile immediately aside the RF antennaassembly 24, curve 144 is for the realized temperature at 1.5 metersradial distance away from the axis of the RF antenna assembly 24, curve146 is for 1.75 meters radial distance, and curve 148 is for 3.5 metersradial distance. 0 meters in the X axis corresponds to antenna feedstructure 50, e.g., the center of the dipole.

Continuing the oil sand test description, the nature of the RF producedhydrocarbon was atypical of the bitumen produced in the oil sand byother process, such as the Clark hot water process or SAGD process.Specifically, RF heating produced a paraffinic oil of considerablyreduced viscosity. As will be appreciated, higher paraffin contenthydrocarbon resources may be considered already upgraded or at or nearpipeline grade as they are thinned with respect to hydrocarbon resourceswith a higher asphalt content, for example. Paraffinic hydrocarbonresources are relatively shiny and transparent or partially so, i.e., awax. In contrast, bitumen typically produced via strip mining and a hotwater bath is jet black and almost solid at −12° C., for example. Higherparaffin content hydrocarbon resources may further be used for refininghigher octane gasoline, for example. Thus, increased paraffin contentmay be valued higher than other types of hydrocarbon resources.

Table 2 compares measured properties of RF produced oil with those oftypical of Clark hot water process bitumen.

TABLE 2 Comparison Of RF Produced Oil With Clark Process Bitumen MiningProcess, RF Process, Method Typical Measured Hydrocarbon Ore Rich OilSand Rich Oil Sand Production Technique Mining, followed by RFstimulated Clark Hot Water well bath separation Produced Oil BaseAsphalt Paraffin API Gravity ~8 ~14 (hydrocarbon relative density)Viscosity in 200,000 39,100 Centipoids, 20° C. Saturates 17% 20%Aromatics 39% 42%After the 35 days of RF heating, and a cool down period that followed, apaddle was dipped into the RF produced oil, which had nearly filled theoversized hole containing the antenna assembly 24. As the oil test wasconducted during cold surface conditions, the temperature of theproduced oil had by the time of sampling cooled to −12 degrees Celsius.In spite of the low −12 Celsius oil measured temperature, the RFproduced oil slowly ran off the paddle. As can be appreciated, the RFproduced oil was thinned and may have been near pipeline gradeviscosity. Several days had elapsed before the oil sample was analyzed.RF produced oil may thicken over time, so the RF produced oil may havehad an even lower viscosity immediately upon completion of the RFheating. Electric and magnetic fields of RF heating cause temporaryaggregation of asphaltene or paraffin particles into larger ones, whichin turn temporarily modifies the rheological properties of the RFproduced oil. The aggregation based thinning may last for a time ofhours, and it is repeatable. Realized thinning times were sufficient forextraction during the RF heating. After the test, oil sand surroundingthe antenna was lighter in color than unheated oil sand nearby.

In oil sand, RF heating with the apparatus 10 produces oil with 3 to 5times more C12 to C28 range molecules than bitumen produced by the ClarkHot Water Process. The lower molecular mass hydrocarbons produced by theapparatus 10 are produced at bulk temperatures of less than about 130°C.: RF electric fields can cause hydrocarbon cracking, and RFelectromagnetic fields (electric and magnetic) are known to causeselective heating of one molecule type over another. Advantageously, theC12 to C28 molecules may be in the valuable diesel and lubricating oilrange.

Referring to FIG. 8, graph 170, an additional method of tuning the balunand dipole comprising the RF antenna assembly 24 will now be described,known here as a method of double tuning. The double tuning method mayadvantageously allow for holding the operating frequency of the RFsource 13 constant throughout the RF heating, as the double tuningmethod provides for increased VSWR bandwidth from the RF antennaassembly 24. For explanation, trace 171 shows the VSWR response versusfrequency of a half wave dipole comprised of the first and secondtubular dipole elements 81a, 81b if no transmission line or common modecurrents were present. This dipole response alone is quadratic or“single dip”. In the double tuning method for the RF antenna assembly24, the balun 15 is included and the spacing s (see FIG. 2) between theproximate ends of the first tubular dipole element 81a and the tubularbalun 15 is varied to produce a double tuned VSWR response depicted astrace 172 in the FIG. 8. The double tuned trace 172 response maycomprise a 4^(th) order Chebyschev polynomial response in someembodiments. A closer spacing s results in a spreading apart of the VSWRminima 174, 176 and an increase in the VSWR bandwidth of the RF antennaassembly 24. A wider spacing s results in a closer spacing of the VSWRminima 174, 176 and a smaller VSWR bandwidth. The double tuning mayprovide a RF antenna assembly 24 VSWR bandwidth that is about 2 to 4times that of the half wave dipole by itself. VSWR ripple amplitude 173will vary with spacing s and is traded for with the VSWR bandwidthrequired.

The double tuning in the RF antenna assembly 24 may result from thecontrolled coupling of two coaxial resonators that exist in situ: 1) theinside surfaces of the first tubular dipole element 81a, and 2) theinside surface of the tubular balun 15. These two structures have theaspects of resonant coaxial stubs that use the outer conductor 71 astheir inner conductor. In other words, the first tubular dipole element81a and tubular balun 15 are coaxial transmission lines over coaxialtransmission lines. Heating a subterranean formation 17 may initiallyincrease formation electrical conductivity due to increased saltconcentration and later decrease conductivity as the liquid watercontent is further eliminated. Changing water content may change heatingapplicator/RF antenna assembly 24 electrical impedance and cause theneed for tunings.

A method of the present embodiments to increase electrical loadresistance is provided by adjusting the ratio of the lengths of thefirst and second tubular dipole elements 81a, 81b. The method may alsoinclude adjusting the first and second tubular dipole elements 81a, 81bin order to make the dipole antenna resistance equal to the transmissionline 82 characteristic impedance. When the RF antenna assembly 24 isinsulated from the subterranean formation 17, making the first andsecond tubular dipole elements 81a, 81b equal in length results in alower or minimum value of electrical resistance. Making the first andsecond tubular dipole elements 81a, 81b unequal in length results in anincreased or higher electrical resistance across the tubular isolator31.

In general, the more conductive the subterranean formation 17 is, thelower the electrical resistance provided by the RF antenna assembly 24,so the more unequal in length the first and second tubular dipoleelements 81a, 81b may be adjusted. Preferred load resistance valuesprovided by the first and second tubular dipole elements 81a, 81b may bebetween about 30 and 70 ohms due to the characteristic impedancesrequired for coaxial transmission lines of lowest loss, highest voltagewithstanding, and or greatest current handling. The resistance versuslength ratio of the first and second tubular dipole elements 81a, 81bmay resemble a tangent function as sine shaped voltage and cosine shapedcurrent relationships may exist. The method for controlling the loadresistance may include using subterranean formation 17 electricalconductivity obtained a priori from well induction resistivity logs,prior to the apparatus 10 installation and completion.

Advantageously, the method allows the apparatus 10 and the RF antennaassembly 24 to heat subterranean formations having a wide range ofelectric conductivities, ranging from about 0.00001 mhos/meterconductivity to 10 mhos/meter and to do so without an undergroundtransformer. As typical, the conductivity of subterranean water can be afunction of dissolved carbon dioxide, which forms weak carbonic acid,OH⁻ radical molecules, and especially any dissolved salts.

Other features relating to apparatuses for RF heating are disclosed inco-pending application “RF ANTENNA ASSEMBLY WITH FEED STRUCTURE HAVINGDIELECTRIC TUBE AND RELATED METHODS,” U.S. patent application Ser. No.13/804,415 filed Mar. 14, 2013, which is incorporated herein byreference in its entirety.

Many modifications and other embodiments of the invention will come tothe mind of one skilled in the art having the benefit of the teachingspresented in the foregoing descriptions and the associated drawings.Therefore, it is understood that the invention is not to be limited tothe specific embodiments disclosed, and that modifications andembodiments are intended to be included within the scope of the appendedclaims.

That which is claimed is:
 1. An apparatus for heating a hydrocarbonresource in a subterranean formation having a wellbore extendingtherein, the apparatus comprising: a radio frequency (RF) source; and anRF antenna assembly configured to be positioned within the wellbore andcoupled to said RF source; said RF antenna assembly comprising a firsttubular dipole element having opposing proximal and distal ends, an RFtransmission line extending through the proximal end of said firsttubular dipole element and comprising an inner conductor, an outerconductor, and a dielectric therebetween, said inner conductor extendingoutwardly beyond the distal end of said first tubular dipole element,said outer conductor coupled to the distal end of said first tubulardipole element, a second tubular dipole element having opposing proximaland distal ends, with the proximal end of the second tubular dipoleelement being adjacent the distal end of said first tubular dipoleelement and being coupled to said inner conductor, and a tubular balunhaving said RF transmission line extending therethrough and opposingproximal and distal ends, with the distal end of the tubular balun beingadjacent the proximal end of said first tubular dipole element and theproximal end of the tubular balun being coupled to said outer conductor.2. The apparatus of claim 1 wherein said RF antenna assembly comprises atubular isolator having said RF transmission line extending therethroughand configured to couple together said tubular balun and said firsttubular dipole antenna element.
 3. The apparatus of claim 2 wherein saidtubular isolator comprises a cyanate ester composite material.
 4. Theapparatus of claim 1 wherein said RF antenna assembly further comprisesa feed structure comprising: a dielectric tube between said first andsecond tubular dipole antenna elements; a first connector coupling saidouter conductor to said first tubular dipole element; and a secondconnector coupling said inner conductor to said second tubular dipoleelement.
 5. The apparatus of claim 4 wherein said first and secondtubular dipole elements each comprises a threaded end; and wherein saidfirst and second connectors each comprises a threaded end engaging arespective threaded end of said first and second tubular dipole elementsfor defining overlapping mechanical threaded joints.
 6. The apparatus ofclaim 4 wherein said first and second connectors each comprises a recessfor receiving adjacent portions of said dielectric tube.
 7. Theapparatus of claim 4 wherein said dielectric tube comprises a cyanateester composite material.
 8. The apparatus of claim 1 wherein said innerconductor comprises a tube defining a first fluid passageway therein;and wherein said outer conductor is spaced from said inner conductor todefine a second fluid passageway.
 9. The apparatus of claim 1 furthercomprising a tubular ferrite choke surrounding said RF transmission lineand spaced apart from the proximal end of said tubular balun.
 10. Theapparatus according to claim 1 wherein said first and second tubulardipole elements have a desired operating frequency; and wherein each ofsaid first tubular dipole element, said second tubular dipole element,and said tubular balun has a length corresponding to +/−10% of a quarterof a wavelength of the desired operating frequency.
 11. An apparatus forheating a hydrocarbon resource in a subterranean formation having awellbore extending therein, the apparatus comprising: a radio frequency(RF) source; an RF antenna assembly configured to be positioned withinthe wellbore and coupled to said RF source; said RF antenna assemblycomprising a first tubular dipole element having opposing proximal anddistal ends, an RF transmission line extending through the proximal endof said first tubular dipole element and comprising an inner conductor,an outer conductor, and a dielectric therebetween, said inner conductorextending outwardly beyond the distal end of said first tubular dipoleelement, said outer conductor coupled to the distal end of said firsttubular dipole element, a second tubular dipole element having opposingproximal and distal ends, with the proximal end of the second tubulardipole element being adjacent the distal end of said first tubulardipole element and being coupled to said inner conductor, a tubularbalun having said RF transmission line extending therethrough andopposing proximal and distal ends, with the distal end of the tubularbalun being adjacent the proximal end of said first tubular dipoleelement and the proximal end of the tubular balun being coupled to saidouter conductor, a tubular isolator having said RF transmission lineextending therethrough and configured to couple together said tubularbalun and said first tubular dipole antenna element, and a feedstructure comprising a dielectric tube between said first and secondtubular dipole antenna elements, a first connector having a firstcircumferential slot for receiving said dielectric tube, and a secondconnector having a second circumferential slot for receiving saiddielectric tube; and a tubular ferrite choke surrounding said RFtransmission line and spaced apart from the proximal end of said tubularbalun.
 12. The apparatus of claim 11 wherein said tubular isolatorcomprises a cyanate ester composite material.
 13. The apparatus of claim11 wherein said first and second tubular dipole elements each comprisesa threaded end; and wherein said first and second connectors eachcomprises a threaded end engaging a respective threaded end of saidfirst and second tubular dipole elements for defining overlappingmechanical threaded joints.
 14. The apparatus of claim 11 wherein saiddielectric tube comprises a cyanate ester composite material.
 15. Theapparatus of claim 11 wherein said inner conductor comprises a tubedefining a first fluid passageway therein; and wherein said outerconductor is spaced from said inner conductor to define a second fluidpassageway.
 16. A method for making a radio frequency (RF) antennaassembly for heating a hydrocarbon resource in a subterranean formationhaving a wellbore extending therein, the method comprising: providing afirst tubular dipole element having opposing proximal and distal ends;positioning an RF transmission line to extend through the proximal endof the first tubular dipole element, the RF transmission line comprisingan inner conductor, an outer conductor, and a dielectric therebetween,the inner conductor extending outwardly beyond the distal end of thefirst tubular dipole element, the outer conductor to be coupled to thedistal end of the first tubular dipole element; providing a secondtubular dipole element having opposing proximal and distal ends, withthe proximal end of the second tubular dipole element being adjacent thedistal end of the first tubular dipole element and coupled to the innerconductor; and positioning a tubular balun to have the RF transmissionline extending therethrough, the tubular balun having opposing proximaland distal ends, with the distal end of the tubular balun being adjacentthe proximal end of the first tubular dipole element and the proximalend of the tubular balun to be coupled to the outer conductor.
 17. Themethod of claim 16 further comprising coupling together the tubularbalun and the first tubular dipole antenna element with a tubularisolator having the RF transmission line extending therethrough.
 18. Themethod of claim 16 further comprising forming a feed structure by atleast: coupling a dielectric tube between the first and second tubulardipole antenna elements; coupling the outer conductor to the firsttubular dipole element using a first connector; and coupling the innerconductor to the second tubular dipole element using a second connector.19. The method of claim 16 further comprising: forming the innerconductor to comprise a tube defining a first fluid passageway therein;and forming the outer conductor to be spaced from the inner conductor todefine a second fluid passageway.
 20. The method of claim 16 furthercomprising positioning a tubular ferrite choke to surround the RFtransmission line and to be spaced apart from the proximal end of thetubular balun.